Aluminous metal brazing materials

ABSTRACT

AN IMPROVED ALUMINUM ALLOY, REFFERED TO AS A CORE MATERIAL, IS PROVIDED WHICH IS PARTICULARLY ADAPTED FOR USE IN MANUFACTURING ARTICLES BY VACUUM BRAZING TECHNIQUES BECAUSE SUCH CORE MATERIAL HAS OPTIMUM RESISTANCE TO SAG AT BRAZING TEMPERATURES AND BECAUSE IT HAS A SOLIDUS OF ABOUT 1160*F. TO 1180*F., IS HEAT TREATABLE TO A MINIMUM YIELD STRENGTH OF 12,000 P.S.I., AND IS CORROSION RESISTANT. A HEAT TREATABLE CLADDING ALLOY IS ALSO PROVIDED FOR USE AS A BRAZING COMPONENT EITHER ALONE OR WITH SUCH CORE MATERIAL AND OTHER SUITABLE CORE MATERIALS. THE PREFERRED CLADDING ALLOY HAS A LIQUIDUS OF ABOUT 10651085*F., HAS A NARROW MELTING RANGE OF ABOUT 20* TO   ABOUT 40*F., IS CORROSION RESISTANT, AND PROVIDES JOINTS OF OPTIMUM STRENGTH AND QUALITY.

1974 I o. R. SINGLETON; JR, ETAL 3,738,824

ALUMINOUS METAL BRAZING MATERIALS Filed Oct. 5, 19.71

FIG-I IIA INVENTORS OGLE R; SINGLETON JR.

BENNIE R. WARD, JR? BY fle @flmluL THEIR ATTORNEYS United States Fatent O 3 788,824 ALUMINOUS META L BRAZING MATERIALS Ogle R. Singleton, Jr., and Bennie Ray Ward, Jr., Richmond, Va., assignors to Reynolds Metals Company,

Richmond, Va. Continuation-impart of abandoned application Ser. No.

18,255, Mar. 10, 1970. This application Oct. 5, 1971,

Ser. No. 186,632

Int. Cl. B32b 15/00 US. Cl. 29197.5 14 Claims ABSTRACT OF THE DISCLOSURE An improved aluminum alloy, referred to as a core material, is provided which is particularly adapted for use in manufacturing articles by vacuum brazing techniques because such core material has optimum resistance to sag at brazing temperatures and because it has a solidus of about 1160 'F. to 1180 F., is heat treatable to a minimum yield strength of 12,000 p.s.i., and is corrosion resistant. A heat treatable cladding alloy is also provided for use as a brazing component either alone or with such core material and other suitable core materials. The preferred cladding alloy has a liquidus of about 1065- 1085 F., has a narrow melting range of about 20 to about 40 F., is corrosion resistant, and provides joints of optimum strength and quality.

BACKGROUND OF THE INVENTION This application is a continuation-in-part of Ser. No. 18,255, filed Mar. 10, 1970, now abandoned.

It is well known in the art that products made from aluminum alloys which have been constructed by vacuum brazing are superior in many respects. In particular, vacuum brazed articles are superior because they do not require the utilization of a special brazing flux which may introduce corrosion problems and requires expensive cleaning operations after brazing. Further, vacuum brazed articles have joint-defining surfaces which are kept relatively free of contamination by reducing the partial pressure of gaseous products and the vacuum environment eliminates contamination of surfaces to be joined by oxides, nitrides, or hydrates, which are usually found in varying amounts even in the best brazing furnaces which do not employ a vacuum environment. The net result is that aluminum joints brazed by vacuum brazing have improved strength and are of optimum quality.

Presently the only two commercially available alumi num alloys which are used extensively as core materials in vacuum brazing are 6951 and 3003 and it is well known that these core materials are not completely satisfactory for the volume production of articles such as heat exchangers, for example. In particular, 6951 alloy (having a solidus of about 1140 F.) sags excessively when brazed at temperatures greater than 1100 F. On the other hand, 3003 alloy which has been used heretofore in vacuum brazing does not tend to sag as much as the 6951; however, 3003 alloy (having a solidus of about 1190 F.) is generally unacceptable in many applications because it is not a heat-treatable alloy. Also, for practical design considerations, 3003 in the temper (as brazed) condition has a yield strength of 6000 p.s.i., and accordingly is not considered an optimum alloy for use in manufacturing high performance heat exchangers of the type used in automobiles, for example.

The alloys which are presently used for cladding 6951 and 3003 core materials generally are completely melted only at temperatures which are too close to the temperature attwhich vacuum brazing is to be accomplished and usually these cladding alloys have a comparatively wide ice melting range which is very undesirable. It has also been found that present cladding alloys do not provide joints of optimum strength for numerous reasons including the great tendency for silicon present in the cladding material to migrate into the core material and the tendency for corrosion in the brazed joint due to the comparatively large dissimilarity between the constituents of commercially available materials and cladding alloys.

Heretofore commercially available aluminum alloys used in vacuum brazing have merely tolerated the presence of iron in the alloy as an impurity. However, it has been found in accordance with the present invention that iron may be deliberately added and controlled as an alloying element to improve the properties of either a core alloy or a cladding alloy.

SUMMARY This invention provides improved aluminum alloys in the form of core alloys or materials and cladding alloys or materials for use in manufacturing articles by vacuum brazing techniques. The compositions of such core and cladding materials are metallurgically and chemically similar enabling these materials to be used in making improved composite constructions such as brazing sheets, for example, which produce high quality structures having optimum corrosion resistance. In addition, the improved core material of this invention has improved resistance to sag at vacuum brazing temperatures, is heat treatable to a minimum yield strength of 12,000 p.s.i., and has a solidus of about 1160 F. to 1180 F. This improved sag resistance at elevated temperatures renders the alloy suitable not only for brazing but also for such other processes as porcelain enameling in which, for example, the core may be clad With relatively pure aluminum.

The preferred cladding material of this invention is completely liquid at a temperature of about 1065-l085 F. and has a narrow melting range of about 20 to about 40 F.

Other details, uses, and advantages of this invention will become apparent as the following description of the embodiments thereof taken in conjunction with the accompanying drawing proceeds.

BRIEF DESCRIPTION OF THE DRAWING The accompanying drawing shows present exemplary embodiments of articles comprising the alloys of this invention and a presentation of sag profiles of such alloys compared with commercial alloys, in which FIG. 1 is a fragmentary perspective view of an exemplary heat exchanger suitable for vacuum brazing using the improved alloys of this invention;

FIG. 2 schematically illustrates sag profiles of sample strips made using exemplary aluminum alloys of this invention compared with sag profiles of sample strips made of 6951 and 3003 alloys wherein such sagging is provided by heating the strips in a vacuum brazing oven;

FIG. 3 is a perspective view with parts in cross section and parts broken away illustrating an exemplary sheet material having both its core and cladding on one surface of the core made of improved aluminum alloys defined in accordane with the teachings of this invention; and

FIG. 4 is a view similar to FIG. 3 illustrating an improved core material provided with improved cladding on opposed surfaces thereof.

DETAILED DESCRIPTION niques and this fact was mentioned earlier. A typical vacuum brazed heat exchanger in the form of an automobile radiator is illustrated in FIG. 1 of the drawing. The radiator has component portions such as its tank 11A, for example, made of a core or composite material of this invention. The lower portion of the tank 11A, i.e., the header 11B, the inside surfaces of the oppositely arranged supporting plates 12, and a major portion of the exposed surfaces of the flattened tubular members 13 may be suitably clad with the improved cladding material of this invention to enable such radiator to be assembled and held together on an associated fixture with its fins 14 in position in any manner, as is well known in the art, and then vacuum brazed at a suitable brazing temperature, for example, at about 1115 F. (preferably controlled within tolerances of plus 25 F. and minus 15 F.).

CORE MATERIALS Although any suitable core alloy or material may be used with the various cladding materials of this invention the preferred core material is an aluminum base alloy having a solidus temperature of about 1160 F. to 1180 F., particularly when such core material is used with a cladding alloy or material of this invention which is completely liquid at about 1065-1085" F. (typically 1075 F.) and has a narrow melting range of about to 40 F. (typically 30 F.). Thus, upon holding the radiator 10 in assembled relation on its fixture and placing it in a commercial brazing oven of known construction which is heated to a suitable brazing temperature, preferably about F. above the liquidus of the cladding and at least 25 F. below the solidus of the core, the component portions thereof are brazed together as one unit.

The following are examples of core alloys or materials of this invention having elements as set forth.

CORE ALLOY EXAMPLE 1 Element: Amount (by weight) Magnesium About 03-06%. Silicon About O.20.5%. Manganese Up to about 0.7%.

Iron About 0.2-0.8%. Chromium Up to about 0.6% Others Each less than .05% with total less than 0.15%.

Aluminum Balance.

CORE ALLOY EXAMPLE 2 Element: Amount (by weight) Magnesium About 0.3-0.6%.

Silicon About 0.2-0.5

Manganese About 0.3-0.7

Iron About 0.2-0.8%.

Chromium Up to about 0.6%.

Others Each less than .05% with total less than 0.15%.

Aluminum Balance.

CORE ALLOY EXAMPLE 3 Element: Amount (by weight) Magnesium About 03-06%. Silicon About 0.2-0.5 Manganese Up to about 0.7%. Iron About 0.20.8%.

Titanium About .01-.10%. Chromium Up to about 0.6%. Others Each less than .05 with total less than 0.15%.

Aluminum Balance.

4 CORE ALLOY EXAMPLE 4 Element: Amount (by Weight) Magnesium About 0.30.6%. Silicon About 0.2-0.5 Manganese Up to about 0.3%.

Iron About 0.2-0.5 Chromium About 0.1-0.6%. Others Each less than .05 with total less than 0.15% Aluminum Balance.

CORE ALLOY EXAMPLE 5 Element: Amount (by weight) Magnesium About 03-06%.

Silicon About O.20.5%.

Manganese About 03-07%.

Iron About O.20.5%.

Chromium About O.1-0.6%.

Others Each less than .05 with total less than 0.15

Aluminum Balance.

As previously indicated, iron is often present in commercially available aluminum alloys and tolerated as an impurity. However, it has been found by extensive tests that iron is effective as an aid in reducing silicon pentration into the core from the molten cladding and thus may be used to provide a core material which has the desired physical qualities. As seen from the above examples of core alloys, iron is preferably controlled so that it constitutes about 02-08% by weight of the alloy. Where chromium is also present, the iron content may be reduced to about 0.2-0.5

Magnesium is provided in the core alloy to assure that desired mechanical property levels may be attained and manganese to assure that the core material has optimum sag resistance at brazing temperature.

Titanium may also be introduced in controlled amounts, especially .01-.10%, as shown in Core Example No. 3, to help control the grain size of the alloy.

As previously indicated, commercially available core materials used in vacuum brazing are 6951 and 3003. 6951 alloy is generally unacceptable for brazing above 1100" F. because it sags excessively, but may be used with the cladding alloys of the present invention for brazing at lower temperatures or with adequate support.

FIG. 2 illustrates the sag profiles of five exemplary test strips or samples which will be designated strips A, B, C, D, and E and the constituent elements and their percentages by weight are shown on the chart which is presented below.

Thick- Percent ofness inch S1 Fe Mn Mg Others Al 0215 22 55 .30 30 15 Balance .022 .37 .75 .01 58 15 Balance 024 .42 67 48 59 15 Balance 022 Commercial 3003 alloy 022 Commercial 6951 alloy Each test sample A-E was 7.865 inches long, 0.750 inch wide, and had a thickness as indicated on the above chart. The samples were supported on a support plate 16 and a horizontal support or pin 17 with approximately 1.865 inches at one end portion of each sample held firmly in a horizontal manner on supports 16 and 17 by a clamping plate 18 and the remaining 6 inches projecting beyond the horizontal pin 17 in a cantilevered manner. The samples A-D were then subjected to a vacuum environment and heated to a temperature of 1125 F. whereby each sample A through D sagged due to heating as shown in FIG. 2.

The sag profile for strip E represents sagging for this strip of 1100 F. when subjected to a similar vacuum environment as the strips A-D. The 1100 F. temperature was selected as the maximum for 6951 alloy because all heat exchanger assemblies made from brazing sheet using 6951 core alloy and brazed at 1100 F. had acceptable sag, but at only slightly higher temperatures of 1105" F.- 1110 P. such assemblies had borderline sag judged unacceptable commercially. Thus, the sag at 1100 F. for sample B using 6951 alloy is considered the base for comparing the exemplary core alloys of this invention and 3003 alloy with 6951 alloy.

It is apparent from FIG. 2 that the core alloys of this invention, A, B, and C are superior in their resistance to sag compared to alloy E and at least as good as alloy D, wherein alloys D and E are commercially available 3003 and 6951 alloys respectively. Sag resistance is important in brazed articles because if there is excessive sag during brazing, it is extremely difiicult to hold manufacturing tolerances and produce sound joints even by using complicated and expensive fixtures.

Although 3003 alloy provides good resistance to sag, it is not heat treatable and has a yield strength of only 6000 p.s.i. in the temper condition. The core alloys of this invention, typified by samples A through C, are heat treatable, i.e., they may be precipitation hardened to achieve a yield strength of at least 12,000 p.s.i.

Thus, it should be emphasized that the improved core alloys of this invention have superior sag resistance to the commercially available 6951 whereby such alloys are particularly adapted for use in vacuum brazing. Further, the core alloys of this invention may be heat treated so that they have a yield strength which is at least about twice the yield strength of 3003, which is the other commercially available aluminum alloy commonly used in vacuum brazing.

CLADDING MATERIALS This invention also provides cladding materials or alloys A which are particularly adapted for use with the core materials having compositions essentially as presented above and such cladding alloys provide superior performance when used with these and other core materials which are to be vacuum brazed. The cladding materials of this invention include those which melt within a narrow range (preferably not exceeding 30 F.) and typically have a liquidus temperature of about 1075 F. Such cladding materials are capable of achieving optimum results with commercially acceptable tolerances at a brazing temperature of about 1115 F.

The following are examples of cladding alloys or materials of this invention having elements as set forth.

CLADDING ALLOY EXAMPLE 1 Element: Amount (by weight) Silicon About 11.0-14.5 Iron About 0.2-l.2%. Chromium Up to about 0.25%. Magnesium About 0.2-1.0%. Others Each less than .05 with total less than 0.15 Aluminum Balance.

CLADDING ALLOY EXAMPLE 2 Element: Amount (by weight) Silicon About 11.0-14.5 Iron About 0.2-1.2%. Chromium Up to about 0.25%. Magnesium About 0.2l.0%. Manganese Up to about 0.3%. Others Each less than .05 with total less than 0.15%.

Aluminum Balance.

6 CLADDING ALLOY EXAMPLE 3 Element: Amount (by weight) Silicon About 11.0-14.5%. Iron About 0.21.2%. Chromium About 0.l0-0.20%. Magnesium About 0.2-1.0%. Manganese Up to about 0.3%. Others Each less than .05% with total less than 0.15%.

Aluminum Balance.

CLADDING ALLOY EXAMPLE 4 Element: Amount (by weight) Silicon About 11.014.5%. Iron About 0.2-1.2%. Chromium Up to about 0.25 Magnesium About 0.2-l.0%. Copper Up to about 0.3%. Others Each less than .05% with total less than 0.15%.

Aluminum Balance.

CLADDING ALLOY EXAMPLE 5 Element: Amount (by weight) Silicon About 11.0-l4.5%. Iron About 0.2-1.2%. Chromium Up to about 0.25%. Magnesium About 0.2-1.0%. Zinc Up to about 0.5%.

Others Each less than .05 with total less than 0.15%. Aluminum Balance.

In addition to the foregoing examples of presently preferred embodiments, other related compositions suitable for use as a brazing component, whether as cladding or in other forms, have been found to include aluminum base alloys consisting essentially of aluminum, about 9-14.5% silicon, about 02-08% iron and about 0.25-0.7% magnesium. Such alloys also may include one or more of the minor alloying elements chromium, manganese, copper and zinc, in amounts up to about 0.25% Cr, 0.5% Mn, 0.3% copper and 0.5% Zn. The silicon content is preferably about 10.5-14.5% when it is desired to achieve a liquidus temperature of about 1065-1 085 F. and a melting range of about 20 to about 40 F., but a lower silicon content may be used when the brazing conditions are less critical.

The following further examples are illustrative of these additional cladding alloys of the present invention:

CLADDING ALLOY EXAMPLE 6 Aluminum Balance, exclusive of incidental elements and minor impurities.

As in the case of the core alloys of this invention, iron, rather than being treated as an impurity in the cladding alloy (as has been done in previous brazing materials),

is introduced as a controlled element. In quantities up to about 1.2% by Weight iron has been found especially effective in controlling viscosity and hence flow of the cladding material consistently with maintaining a narrow melting range of the alloy.

It should also be noted that chromium may be a deliberate alloying element which contributes to brazability and corrosion resistance of the cladding when used in the range of up to about 0.25% of the composition. However, it has been found that chromium in the controlled range of 0.10-0.20%( by weight provides the best results. For some uses, up to about 0.5% manganese may be added as a deliberate alloying element, with or Without chromium, in others up to about 0.3% copper, and in still others, up to about 0.5 zinc. Magnesium has been added to control the mechanical properties of the cladding alloy, but the amount is limited to improve bonda-bility. Copper and zinc in the amounts indicated are used respectively to control wettability and galvanic potential.

The amount of silicon in the cladding alloy may be in the range of about 9-14.5% of the total weight of the composition, but is preferably at least about 10.5% for reasons previously mentioned. The amount of silicon is important in that it is known that silicon diffusion or migration from the cladding material or alloy into the core material or alloy is harmful. The reduction of silicon in the cladding material has the effect, in hypoeutectic silicon alloys, of raising .the liquidus temperature. The higher the liquidus temperature the less. the flow at a given brazing temperature.

It has been found in accordance with the present invention that adding at least about 0.3% manganese by weight in the core tends to resist this silicon diffusion into the core material whereby a resulting article or structure formed utilizing both the core material and cladding of this invention exhibits optimum properties especially compatible with vacuum brazing. Thus, by precise control of the amount of silicon to achieve the desired melting range of the cladding alloy, and by use of manganese in the core to help control silicon diffusion, an improved brazing material has been provided by this invention.

The core and cladding alloys or materials of this invention may be made in any form and used in any manner, including those known in the art, and either with each other or with commercially available materials or alloys. For example, the core alloys may be produced in any suitable form, such as tube, rod, sheet, etc.; and, the cladding alloys may be made as separate articles such as O-rings, stn'ps, discs, wire, etc., which are mechanically held against or between a pair of component members which are to be joined by brazing.

Preferably, the cladding materials or alloys are each provided in the form of cladding, in layer form, on an article such as a composite or brazing sheet 20 having a plurality of layers, as shown in FIG. 3. The exemplary sheet 20 is comprised of a core alloy 21 which may have constituent elements as presented in any of the above examples and such sheet has a cladding alloy 22 clad on one side thereof. The alloy 22 may have constituent elements essentially as presented above.

A brazing sheet may also be provided essentially a illustrated in FIG. 4 of the drawing and designated generally by the reference numeral 20A. The brazing sheet 20A may be comprised of a core material 21 made with constituent elements as outlined above and may be provided with cladding 22 on both sides thereof with the cladding alloy 22 also having constituent elements as outlined above.

The thickness of the cladding which is provided on a given sheet, such as the sheet 20 or 20A will vary, depending upon the overall thickness of the composite sheet. For production sheets particularly adapted for use in vacuum brazing having a composite or total thickness of 0.024 inch or less, the cladding thickness on a side may be about of the overall thickness; for sheets 0.025

inch to 0.063 inch, the cladding thickness on a side may be about 8% of the composite thickness; and, for sheets having a composite thickness of 0.064 inch and above the cladding thickness on a side may be about 4% of the composite thickness. The above percentages of cladding thickness are typically applied regardless of whether one or both sides of the sheet are clad.

The ratio of the thickness of the cladding to the thickness of the core may be varied to suit the joining conditions without appreciably changing the strength of the resulting product. It will also be apparent from a detailed comparison of constituent elements of the core and cladding that the composition of the cladding and the core are metallurgically and chemically similar, thereby providing a system which has excellent corrosion resistance. The composite construction, such as sheets 20 and 20A, defined by a core alloy of this invention clad with a cladding alloy as taught herein also resists silicon migration from the cladding into the core to a greater extent than any previously known heat treatable brazing sheet composite; further, the composite construction has unexpectedly high resistance to sag during preheating for vacuum brazing and may be heat treated to provide yield strengths of 12,000 psi.

The composite sheet construction of this invention also exhibits the greatest spread of temperature between cladding liquidus and core solidus of any heat treatable brazing composite known heretofore. In particular, and as has been pointed out earlier, the preferred cladding alloy is completely liquid at about 1065-1085" F. while the solidus of the core material is about 1160 F. to 1180 F., whereby a minimum temperature spread of approximately 75 F. is provided. This large temperature spread between solidus of the core alloy and liquidus of the cladding alloy enables commercial vacuum brazing furnaces to be equipped with less sophisticated and hence comparatively inexpensive temperature controls.

In this example of the invention, an exemplary heat exchanger 10 has been shown as being made utilizing an improved core alloy and an improved cladding alloy as taught by this invention; however, it is to be understood that any suitable product may be made from the unique alloys as taught by this invention.

Articles in the form of sheets 20 and 20A have been illustrated in FIGS. 3 and 4 respectively merely as examples of composite constructions each using core and cladding alloys of this invention. However, it will be appreciated that composite constructions having any form, shape, etc., may be made using the alloys of this invention.

While present examplary embodiments of this invention, and methods of practicing the same, have been illustrated and described, it will be recognized that this invention may be otherwise variously embodied and practiced within the scope of the following claims.

What is claimed is: 1. An article comprising a clad composite having a core and a brazing component in the form of a cladding on said core, wherein:

said cladding is composed of an aluminum base alloy consisting essentially of aluminum, about 11-l4.5% Si, about 02-12% Fe, up to about 0.25% Cr, up to about 0.3% Mn and about 0.2-0.1% Mg, by weight; and

said core is composed of an aluminum base alloy consisting essentially of aluminum, about 03-06% Mg, about 0.20.5% Si, up to about 0.6% Cr, up to about 0.7% Mn and about 0.2-0.8% Fe, by weight.

2. An article according to claim 1 in the form of a composite sheet.

3. An article according to claim 1 in which the manganese content of said core alloy is at least 0.3% by weight.

4. An article comprising a clad composite having a 9 core and a brazing component in the form of a cladding on said core, wherein:

said cladding is composed of an aluminum base alloy consisting essentially of aluminum, about 11-14.5% Si, about 0.21.2% Fe, up to about 0.25% Cr, up to about 0.3% Mn and about 0.21.0% Mg, by weight; and

said core is composed of an aluminum base 'alloy consisting essentially of aluminum, about 0.3-0.6% Mg, about 02-05% Si, up to about 0.6% Cr, up to about 0.7% Mn, about .01-0.l% Ti and about 0.2- 0.8% Fe, by weight.

5. An article according to claim 1 in which said cladding is adhered to a core composed of an aluminum base alloy consisting essentially of aluminum, about 0.30.7% Mn, about 0.3-0.6% Mg, about 0.20.5% Si, about 0.1- 06% Cr, and about 0.2-0.5% Fe by weight.

6. An article comprising a clad composite having a core and brazing component in the form of a cladding on said core, wherein:

said cladding is composed of an aluminum base alloy consisting essentially of aluminum, about 914.5% Si, about 0.2-0.8% Fe and about 0.25-0.7% Mg, by weight; and

said core is composed of an aluminum base alloy consisting essentially of aluminum, about 0.3-0.6% Mg, about 0.20.5% Si, up to about 0.7% Mn, up to about 0.6% Cr and about 0.2-0.8% Fe, by weight.

7. A heat treatable clad composite comprising a core alloy consisting essentially of aluminum, about 0.3-0.6% Mg, about 0.20.5% Si, about 0.2-0.8% Fe, up to about 0.6% Cr, and up to about 0.7% Mn by weight, said core alloy having a solidus temperature of about 1160 F. to 1180 F.; and a cladding alloy clad on said core alloy and consisting essentially of aluminum, about 10.5-14.5 Si, about 0.21.2% Fe, up to about 0.3% Mn, up to about 0.25% Cr, and about 0.21.0% Mg by weight, said cladding alloy having a melting range of about 20 to about 40 F. and a liquidus temperature of about 8. A composite as set forth in claim 7 in the form of a sheet having a plurality of layers with one layer being defined by said core alloy and at least one layer being defined by said cladding alloy.

9. A composite as set forth in claim 7 in which said core alloy is heat treatable to a minimum yield strength of 12,000 psi.

10. A heat treatable clad composite comprising a core alloy consisting essentially of aluminum, about 0.3-0.6% Mg, about 0.20.5% Si, about 0.2-0.8% Fe, up to about 0.6% Cr, and up to about 0.7% Mn by 'weight, said core 10 alloy having a solidus temperature of about 1160 F. to 1180 F.; and a cladding alloy clad on said core alloy and consisting essentially of aluminum, about 9-14.5% Si, about 0.20.8% Fe, up to about 0.5% Mn, up to about 0.25% Cr, up to about 0.3% Cu, up to about 0.5% Zn, and about 0.25-0.7% by Weight.

11. In a clad composite brazing sheet of the type having a core composed of aluminum alloy 6951 and an Al-Si cladding on said core, the improvement wherein said cladding consists essentially of aluminum, about 9- 14.5 Si, about 02-08% Fe and about 0.25-0.7% Mg, by weight, with incidental elements and impurities in amounts up to about 0.25% Cr, 0.5 Mn, 0.3% Cu and 0.5 Zn, others less than .05% each and 0.15% total.

12. In a clad composite brazing sheet of the type having a core composed of aluminum alloy 3003 and an Al-Si cladding on said core, the improvement wherein said cladding consists essentially of aluminum, about 9- 14.5% Si, about 0.2-0.8% Fe and about 0.25-0.7% Mg, by weight, with incidental elements and impurities in amounts up to about 0.25 Cr, 0.5 Mn, 03% Cu and 0.5 Zn, others less than .05 each and 0.15 total.

13. In a clad composite brazing sheet of the type having a core composed of aluminum alloy 6951 and an Al-Si cladding on said core, the improvement wherein said cladding consists essentially of aluminum, about 11- 14.5% Si, about 0.21.2% Fe, up to about 0.25% Cr, up to about 0.3% Mn and about 0.21.0% Mg, by weight.

14. In a clad composite brazing sheet of the type having a core composed of aluminum alloy 3003 and an Al-Si cladding on said core, the improvement wherein said cladding consists essentially of aluminum, about 11- 14.5 Si, about 0.21.2% Fe, up to about 0.25% Cr, up to about 0.3% Mn and about 0.21.0% Mg, by weight.

References Cited UNITED STATES PATENTS 2,602,413 7/1952 Miller 29-1975 2,821,014 1/1958 Miller 29-1975 3,168,381 2/1965 Finnegan 29-1975 3,290,129 12/1966 Nock 29-1975 3,372,008 3/1968 Korver 29-1975 3,496,620 2/ 1970 Wolfe 29-1975 3,553,825 1/1971 Dockus 29-1975 OTHER REFERENCES Metals Handbook by American Society of Metals, published 1961, vol. 1, p. 917.

HYLAND BIZOT, Primary Examiner 5333 UMTEB STATES PATENT GFFICE Q1? .TEFEQATE U35 CQRHEQTKQN Dated Jan. 29 1974 Inventor) "O R. slngleton Jro and Bennle Ray Ward, Jr.

the abcve identified patent It is certified that error appears in as shawl below:

and that said Letters Patent are hereby corrected Column 8, line 63, for "OJ-0.1%", read 0,,2-l.O

Column 10 line 6 for "O 25-0 7% by weight read 0 25-9 7% Mg by weight Signed and sealed this 11th day of February 1975.

(SEAL) Attest Cu MARSHALL DANN 'RUTH C. MASON Attesting Gfficer Cdmissioner of Patents and Trademarks 

